JPH04501087A - How to manufacture a crown for an articulated piston - Google Patents

How to manufacture a crown for an articulated piston

Info

Publication number
JPH04501087A
JPH04501087A JP89501366A JP50136689A JPH04501087A JP H04501087 A JPH04501087 A JP H04501087A JP 89501366 A JP89501366 A JP 89501366A JP 50136689 A JP50136689 A JP 50136689A JP H04501087 A JPH04501087 A JP H04501087A
Authority
JP
Japan
Prior art keywords
crown
side wall
top surface
ring groove
machining
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP89501366A
Other languages
Japanese (ja)
Other versions
JP2801049B2 (en
Inventor
アダムス マーシャル
レックナー ジェリー エム
Original Assignee
キャタピラー インコーポレーテッド
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by キャタピラー インコーポレーテッド filed Critical キャタピラー インコーポレーテッド
Publication of JPH04501087A publication Critical patent/JPH04501087A/en
Application granted granted Critical
Publication of JP2801049B2 publication Critical patent/JP2801049B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/10Making specific metal objects by operations not covered by a single other subclass or a group in this subclass pistons
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/0015Multi-part pistons
    • F02F3/0069Multi-part pistons the crown and skirt being interconnected by the gudgeon pin
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49249Piston making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49249Piston making
    • Y10T29/49252Multi-element piston making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49249Piston making
    • Y10T29/49265Ring groove forming or finishing
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988Metal casting
    • Y10T29/49989Followed by cutting or removing material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49995Shaping one-piece blank by removing material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49995Shaping one-piece blank by removing material
    • Y10T29/49996Successive distinct removal operations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Forging (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるため要約のデータは記録されません。 (57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 関節式ピストン用のクラウンを製造する方法技術分野 本発明は、2部品式ピストンのクラウンを製造する方法、一層詳しくは、完成し たクラウンを機械加工する方法に関する。[Detailed description of the invention] How to manufacture crowns for articulated pistonsTechnical field The present invention relates to a method for manufacturing a two-part piston crown, and more particularly to a method for manufacturing a two-part piston crown. This invention relates to a method for machining a crown.

背 景 過去数年にわたるエンジンの開発で、エンジンの排気量を増大させることなく馬 力が向上した。この馬力の向上のためには、ピストンを介して連接棒に伝えられ る燃焼室内燃焼圧力を増大させる必要があった。background Engine development over the past few years has enabled the horse to be powered without increasing engine displacement. Strength has improved. In order to increase this horsepower, the power is transmitted to the connecting rod through the piston. It was necessary to increase the combustion pressure in the combustion chamber.

燃焼圧力の増大には、ピストンの一体性を改善して増大した応力に耐えるように しなければならない。過去にも、また、今日の多くのケースでも、ピストンはア ルミニウムまたは鋳鉄で作られている。ここに述べるピストンというのは、2部 品量節式ピストンの、鍛造で機械加工したクラウンを設けることによって増大し た圧力に耐える要件を満たしているものとする。鍛造材料は5AE4140であ り、クロムとモリブデンを含む合金鋼である。Increased combustion pressure requires improved piston integrity to withstand the increased stress. Must. In the past, and in many cases today, pistons Made of aluminum or cast iron. The piston described here has two parts. Increased by the forged and machined crown of the low-volume piston. shall meet the requirements for withstanding pressure. The forging material is 5AE4140. It is an alloy steel containing chromium and molybdenum.

より高級な鋼のピストン・クラウンを開発しているときに、機械加工がきわめて 難しい材料が発見された。この材料はきわめて強靭であるため、工具のガミング を生じさせる性質があり、独特な機械加工法を開発する必要があった。これが本 発明の主題である。While developing higher grade steel piston crowns, machining was extremely difficult. A difficult material has been discovered. This material is extremely tough and prevents tool gumming. It is necessary to develop a unique machining method. this is the book is the subject of the invention.

発明の開示 本発明の一局面によれば、関節式ピストンのクラウンを製造する方法が提供され る。このクラウンは、円形の頂面と、この頂面から下方に延びる燃焼クレータと 、頂面から下方に延び、円筒形の表面を有する側壁とを有する。側壁には、複数 のリング溝が設けてあり、これらのリング溝は頂面から下方に間隔を置いて位置 している。側壁は頂面および燃焼クレータ付近まで延びる冷却ギヤラリの第1側 部を形成する内面を有する。垂れ下がった中央部を貫通して側方に延びるビン受 は孔が形成してあり、また、クレータ付近の面が冷却ギヤラリの第2壁面を形成 している。側壁はその中央部と冷却ギヤラリの間に延びる底面を有し、この底面 はビン受は孔の上方に位置している。Disclosure of invention According to one aspect of the invention, a method of manufacturing a crown for an articulated piston is provided. Ru. This crown has a circular top surface and a combustion crater extending downward from the top surface. , and a side wall extending downwardly from the top surface and having a cylindrical surface. On the side wall, there are several These ring grooves are located at intervals downward from the top surface. are doing. The side wall is the first side of the cooling gear that extends to the top surface and near the combustion crater. It has an inner surface forming a section. A bottle holder that extends laterally through the hanging central part. A hole is formed in the hole, and the surface near the crater forms the second wall surface of the cooling gear gallery. are doing. The side wall has a bottom surface extending between the central portion thereof and the cooling gear gallery, and the bottom surface The bottle holder is located above the hole.

機械加工段階は次の通りである。側壁の外面、リング溝、頂面および燃焼クレー タを粗加工する。次の段階で、クラウンの底面を仕上げ加工する。次いで、クラ ウンを保持装置から外し、チャック部材をビン受は孔に挿入する。次に、クラウ ンをその底面を止めに当て、冷却ギヤラリの片面がロケータに当たるように位置 決めする。これにより、クラウンは仕上げ作業に合わせて位置したことになり、 この位置を保ったまま、燃焼クレータ、頂面、リング溝および側壁の円筒形外面 を仕上げ加工することができる。The machining steps are as follows. External surface of side wall, ring groove, top surface and combustion clay Roughly process the data. The next step is to finish the bottom of the crown. Next, the club Remove the bottle from the holding device and insert the chuck member into the bottle holder hole. Next, Crow Position the cooling gear so that its bottom is against the stop and one side of the cooling gear is against the locator. Decide. This ensures that the crown is in position for finishing work. While maintaining this position, the cylindrical outer surface of the combustion crater, top surface, ring groove and side wall can be finished.

本発明の第2の局面は、外面の成る部分をチャックで把持し、この外面の粗加工 を行い、■・つのリング溝の位置に重なった領域でこの作業を終了する粗加工方 法である。次いで、クラウンをチャックから外し、機械加工済みの面に再挿入し 、残った材料を外面から除去し、次いで、リング溝を加工し、切断を中断したと ころに連結部を残す。A second aspect of the present invention is to grip a portion of the outer surface with a chuck and perform rough processing on the outer surface. ■・Rough machining method that finishes this work in the area that overlaps the position of the two ring grooves. It is the law. The crown is then removed from the chuck and reinserted onto the machined surface. , the remaining material was removed from the outer surface, then the ring groove was machined and the cutting was interrupted. Leave a connecting part on the roller.

前記の局面および他の局面は添付図面に関連した以下の説明から明らかとなろう 。特に、図面が発明の限定を意図したも9ではなく、はんの例示の目的で描いた ものであることは了解されたい。The above and other aspects will become apparent from the following description in conjunction with the accompanying drawings. . In particular, the drawings are drawn for illustrative purposes and not for purposes of limitation. Please understand that this is a thing.

図面の簡単な説明 第1図は2部品関節式ピストンの横断面図であり、ここでは、クラウンを断面で 示し、スカート、連接棒およびピストン・ビンを破線で示しである。Brief description of the drawing Figure 1 is a cross-sectional view of a two-part articulated piston, where the crown is shown in cross-section. The skirt, connecting rod and piston pin are shown in dashed lines.

第2図は2部品関節式ピストンのクラウンを製造する段階の概略図である。FIG. 2 is a schematic diagram of the steps in manufacturing the crown of a two-part articulated piston.

発明を実施するための最良の形感 第1図において、ここには、2部品関節式ピストン1oが示しである。この2部 品関節式ピストンは、断面で示すクラウン11と、破線で示す付属のスカート1 2とを包含する。クラウンおよびスカートはピストン・ビン16によって連接棒 14に取り付けられる。連接号14は図示しないエンジンのクランク軸に取り付 けられる。The best form for carrying out inventions In FIG. 1, a two-part articulated piston 1o is shown. This second part The articulated piston has a crown 11 shown in cross section and an attached skirt 1 shown in broken lines. 2. The crown and skirt are connected to the connecting rod by piston pin 16. 14. Connection number 14 is attached to the crankshaft of the engine (not shown). I get kicked.

クラウン11は円形の頂面18と、この頂面18から下方に延びる燃焼クレータ 20とを育する。頂面18からは円形の側壁22が下方に延びており、この側壁 は円筒形の外面24を存する。The crown 11 has a circular top surface 18 and a combustion crater extending downward from the top surface 18. Cultivate 20. A circular side wall 22 extends downward from the top surface 18; has a cylindrical outer surface 24.

円筒形の外面24から側壁22内へ複数のリング溝26が延びており、これらの リング溝は頂面18の下方において間隔を置いて位置している。A plurality of ring grooves 26 extend from the cylindrical outer surface 24 into the side wall 22; The ring grooves are spaced below the top surface 18.

側壁22は内面28を存し、この内面は内部冷却ギヤラリ30の第1側面を構成 する。下方のリング溝27の底から冷却ギヤラリ30に向かってドレン通路27 が延びている。内面28は頂面18と燃焼クレータ30の付近まで上方に延びて いる。垂れ下がり中央部32が燃焼クレータ20および頂面18の下方の隣接し た位置から下方に延びていて一対のボス34を構成している。各ボスを貫いてピ ン受は孔36が形成してあり、このピン受は孔はピストン・ビン36を受ける連 続したビン孔と整合している。ブッシング37がピン受は孔にプレス族めしであ る。冷却ギヤラリ30の第2側面38は、中央部32の、頂面18の下方、燃焼 クレータ20付近で始まる面で与えられる。The side wall 22 has an inner surface 28 that constitutes a first side of the internal cooling gearing 30. do. The drain passage 27 extends from the bottom of the lower ring groove 27 toward the cooling gear gallery 30. is extending. The inner surface 28 extends upwardly to the vicinity of the top surface 18 and the combustion crater 30. There is. The depending central portion 32 is adjacent to the combustion crater 20 and below the top surface 18. A pair of bosses 34 extend downward from the position shown in FIG. Piercing through each boss The pin receiver has a hole 36 formed therein, and the hole is connected to receive the piston pin 36. It is consistent with the continuous bottle hole. The bushing 37 has a pin holder that is pressed into the hole. Ru. The second side 38 of the cooling gearing 30 is located in the central portion 32, below the top surface 18, It is given by a plane starting near crater 20.

側壁22は円筒形面24と冷却ギヤラリ30の間に延びる底面40を有する。こ の底面40は、ピン受は孔36の上方、一層詳しく言えば、ピン受は孔の上方円 形面に対して接線方向の水平面上方に位置する。Sidewall 22 has a bottom surface 40 extending between cylindrical surface 24 and cooling gearbox 30 . child The bottom surface 40 of the pin receiver is located above the hole 36, more specifically, the pin receiver is located above the hole Located above the horizontal plane tangential to the shape.

次に第2図を参照して、上述したクラウンを製造する第1段階は、クロム・モリ ブデン合金からなる鋼合金材料のビレットの鍛造である。この材料は5AE40 41に記載されている組成物であり、炭素、マンガン、燐、硫黄、シリコン、ク ロム、モリブデン、残余鉄および痕跡元素からなる。Next, referring to FIG. 2, the first step in manufacturing the above-mentioned crown is to It is a forged billet of steel alloy material made of buden alloy. This material is 5AE40 41, and contains carbon, manganese, phosphorus, sulfur, silicon, and carbon. Consists of rom, molybdenum, residual iron and trace elements.

ビレットは、次に、プレス内に置き、ダイによってほぼピストン・クラウンの形 状に鍛造する。このとき、後述の2段階機械加工過程を可能とするに充分な材料 が与えられる。The billet is then placed into a press and shaped approximately into a piston crown by a die. Forged into shape. At this time, sufficient material is available to enable the two-step machining process described below. is given.

本発明の一局面において、第1段階で、クラウンを旋盤内にあるいはボスを機械 加工センタにチャック止めすることによって位置決めし、側壁の外面を機械加工 できるように露出させておく。In one aspect of the invention, the first step is to place the crown in a lathe or machine the boss. Position by chucking to the machining center and machining the outer surface of the side wall. Leave it as exposed as possible.

この段階で、クラウンを粗加工して頂面18、クレータ20、側壁の円筒形外面 およびリング溝を製作する。下方リング溝に入れるオイル・リングのためのドレ ン通路をこの段階でドリル加工しても良い。At this stage, the crown is rough-machined to form the top surface 18, the crater 20, and the cylindrical outer surface of the side wall. and make a ring groove. Drain for oil ring to lower ring groove You may drill the passageway at this stage.

この第1段階の別の方法としては、側壁の鍛造した外面をチャック止めし、その 一部を粗加工し、リング溝の1つと重なる領域において切削を中断するという方 法もある。次いで、クラウンをチャックから外し、粗加工面を再チャック止めす る。上述した残りの表面を粗加工してから、1つのリング溝に重なる領域で円筒 形側壁への切削を中断し、次いで、粗削りを行ってリング溝を切削し、切削中断 時に生じた表面の結合部を取り除く。An alternative method for this first step is to chuck the forged outer surface of the sidewall and For those who roughly machine a part and interrupt cutting in the area that overlaps with one of the ring grooves. There is also a law. Next, remove the crown from the chuck and chuck the rough machined surface again. Ru. Roughly machine the remaining surfaces as described above, then cut the cylinder in the area that overlaps one ring groove. Cutting to the side wall of the shape is interrupted, then rough cutting is performed to cut the ring groove, and cutting is interrupted. Remove any surface bonds that may have formed during the process.

粗加工作業中、はぼ0.030インチ(0,75mm)の材料を仕上げ加工作業 のために残す。During rough machining, finish machining of 0.030 inch (0.75 mm) material leave for.

次の段階で、クラウンを円筒形外面上にチャック止めし・機械加工用にピストン の下面を露出させる。この段階で、底面40および冷却ギヤラリ30の壁面を、 ボス34にピン受は孔36を明けたと同様に加工する。In the next step, the crown is chucked onto the cylindrical outer surface and the piston is prepared for machining. expose the bottom side of the At this stage, the bottom surface 40 and the wall surface of the cooling gear gallery 30 are The pin receiver is machined in the same way as the hole 36 is drilled in the boss 34.

次の段階で、ブッシング37をピン受は孔36内にプレス族めし、エンジンに組 み込むときにピストン・ビンに適合する寸法まで仕上げ加工する。In the next step, the bushing 37 is pressed into the pin hole 36 and assembled into the engine. Finish machining to the dimensions that fit the piston bottle when inserting.

次の段階で、バーまたはチャック部材をピン受は孔に挿入し、これを機械チャッ ク内でドローパーによって把持する。ピストン・クラウンの底面40はチャック のフェースプレートまたはロケータに向かって引く。これにより、クラウンが最 終加工作業のためにチャック上の芯合わせ位置に位置する。In the next step, the bar or chuck member is inserted into the hole of the pin receiver and this is inserted into the mechanical chuck. grip with a drawper inside the box. The bottom surface 40 of the piston crown is a chuck faceplate or locator. This will ensure that the crown is Located in centering position on the chuck for finishing operations.

仕上げ加工作業の後、クラウンをチャックから外し、最終的な組み立ての準備を することができる。 クレータ、頂面、円筒形外面およびリング溝についてのこ の2段階機械加工により、工具跡や他の欠陥のない仕上げ面を得ることができる 。このような欠陥はクラウンの一体性を壊すことになるなんらかの亀裂を伝播す る可能性がある。After finishing operations, the crown is removed from the chuck and prepared for final assembly. can do. About the crater, top surface, cylindrical outer surface and ring groove The two-step machining process provides a finished surface free of tool marks and other defects. . Such defects may propagate some kind of crack that will destroy the integrity of the crown. There is a possibility that

上記の方法は冷却ギヤラリを仕上げる処理段階や鍛造過程のための段階を含まな い。The above method does not include a processing step for finishing the cooling gear or a step for the forging process. stomach.

本発明の他の局面、目的および利点は本明細書、図面および添付請求の範囲を研 究することから明らかとなろう。Other aspects, objects, and advantages of the invention may be found in the specification, drawings, and appended claims. This will become clear through investigation.

第2図 国際調査報告 l詐−−Gs+I@m−ム―−に一1’−N−、PCT/us88104605 1III@fit−IIal^ee+=−1,−−−PCT/US 88104 605−階一一^−−減一神* pcTlus 88104605国際調査報告Figure 2 international search report 1'-N-, PCT/us88104605 1III@fit-IIal^ee+=-1, ---PCT/US 88104 605-Kai 11^--Reduced One God *pcTlus 88104605 International Investigation Report

Claims (1)

【特許請求の範囲】 1.関節式ピストン(10)のクラウン(11)であって、円形の頂面(18) 、この頂面から下方に延びる燃焼クレータ(20)、頂面(18)から垂れ下が り、円筒形の外面(24)を有する側壁(22)および側壁(22)に設けてあ り、頂面(18)の下方の間隔を置いた位置に配置した複数のリング溝(26) を有するクラウン(11)であり、側壁(22)が、冷却ギャラリ(30)の、 頂面(18)および燃焼クレータ(20)付近まで延びる第1側面を形成す内面 (28)と、側方に貫通するピン受け孔(36)を有する垂れ下がり中央部(3 2)とを有し、この中央部(32)が冷却ギャラリ(30)の第2側面(38) を形成する表面を有し、側壁(22)がそれと冷却ギャラリ(30)の間に延在 し、ピン受け孔(36)上方に位置する底面(40)を有するクラウン(11) を製造する方法であって、 a.側壁(22)の円筒形外面(24)、リング溝(26)、頂面(18)およ び燃焼クレータ(20)を粗加工する段階と、b.クラウン(11)の底面(4 0)を仕上げ加工する段階と、 c.ピン受け孔(36)を通して或る部材を挿入し、クラウン(11)の底面( 40)を止めに当てがい、冷却ギャラリ(30)の片側(28、38)をろけえ たに当てがってクラウン(11)を位置決めする段階と、 d.クラウン(11)を位置決めしながら燃焼クレータ(20)、頂面(18) 、リング溝(26)、側壁(22)の円筒形外面(24)を仕上げ加工する段階 とを包含することを特徴とする方法。 2.請求の範囲第1項記載の方法において、鋼合金のビレットからクラウン(1 1)をほぼ完成クラウンの形状に鍛造し、粗加工段階、仕上げ加工段階のために 充分な材料を残す段階を包含することを特徴とする方法。 3.請求の範囲第2項記載の方法において、鋼合金が、炭素、マンガン、燐、硫 黄、シリコン、クロム、モリブデン、残余鉄および痕跡元素からなることを特徴 とする方法。 4.請求の範囲第1項記載の方法において、粗加工段階後に約0.030インチ (0.75mm)の材料が残り、仕上げ加工段階で除去されることを特徴とする 方法。 5.請求の範囲第1項記載の方法において、粗加工段階がボス(34)をチャッ クで締め付けることによってクラウン(11)を保持する段階を含むことを特徴 とする方法。 6.請求の範囲第1項記載の方法において、粗加工段階が、a.側壁(22)を その一端付近で把持し、その円筒形外面(24)の、側壁(22)の別の端と1 つのリング溝(26)の位置と重なる領域との間の部分を機械加工する段階と、 b.円筒形外面(24)の前記粗加工した部分を把持し、側壁(22)の円筒形 外面(24)の、前記一端と1つのリング溝(26)の前記重なる領域の間の残 りの部分を粗加工する段階と、 c.側壁(22)に前記1つのリング溝(26)を切削し、段階a、bの粗加工 作業の任意の連結部を除去する段階と、d.前記リング溝(26)の残りを切削 する段階とを包含することを特徴とする方法。 7.請求の範囲第1項記載の方法において、さらに、ボス(34)にピン受け孔 (36)を粗加工する段階と、 b.ピン受け孔(36)を仕上げ加工する段階と、c.仕上げたピン受け孔(3 6)にブッシング(37)を組み込む段階と、 d.請求の範囲第1項の段階cの前に組み込んだブッシング(37)の内径をを その仕上げ直径まで機械加工する段階とを包含することを特徴とする方法。 8.関節式ピストン(10)のクラウン(11)を機械加工する方法であって、 円形の頂面(18)、この頂面(18)から下方に延びる燃焼クレータ(20) 、頂面(18)から垂れ下がり、円周形の外面(24)を有する比較的短い側壁 (22)および側壁(22)に設けてあり、頂面(18)の下方で間隔を置いた 位置に配置した複数のリング溝(26)を有するクラウン(11)であって、側 壁(22)が頂面(18)および燃焼クレータ(20)に隣接して延びる冷却ギ ャラリ(30)の第1側面を形成する内面(28)と、側方に貫通するピン受け 孔(36)を有する垂れ下がった中央部(32)とを有し、側壁(22)が円筒 形側壁(22)と冷却ギャラリ(30)の間に延在し、ピン受け孔(36)の上 方に位置する底面(40)を有するクラウン(11)を機械加工する方法におい て、 a.側壁(22)をその一端付近で把持し、その円筒形外面(24)の、側壁( 22)の別の端と1つのリング溝(26)の位置と重なる領域との間の部分を粗 加工する段階と、b.外面(24)の前記粗加工した部分を把持し、側壁(22 )の円筒形外面(24)の、前記一端と前記1つのリング溝(26)の前記重な り領域の間の別の部分を粗仕上げする段階と、 c.側壁(22)に前記1つのリング溝(26)を切削し、段階a、bの粗仕上 げ作業で残った任意の連結部を除去する段階と、 d.前記リング溝(26)の残りを切削する段階と包含することを特徴とする方 法。 9.請求の範囲第8項記載の関節式ピストンのクラウンを機械加工する方法にお いて、さらに、 a.頂面(18)、燃焼クレータ(20)および底面(40)を粗加工する段階 と、 b.クラウン(11)の底面(40)を仕上げ加工する段階と、 c.垂れ下がり中央部(32)を貫いて側方に延びるピン受け孔(36)を機械 加工する段階と、d.ピン受け孔(36)に或る部材を挿入し、底面(40)を 止めに当てがい、冷却ギャラリ(30)の片面をロケータに当てがってクラウン (11)を位置決めする段階と、e.クラウン(11)を位置決めしながら燃焼 クレータ(20)、頂面(18)、円筒形外面(24)およびリング溝(26) を仕上げ加工する段階と を包含することを特徴とする方法。[Claims] 1. Crown (11) of the articulated piston (10), the circular top surface (18) , a combustion crater (20) extending downward from the top surface, and a combustion crater (20) that hangs down from the top surface (18). and a side wall (22) having a cylindrical outer surface (24) and provided on the side wall (22). a plurality of ring grooves (26) arranged at spaced positions below the top surface (18); a crown (11) having a side wall (22) of a cooling gallery (30); an inner surface forming a first side surface extending to the vicinity of the top surface (18) and the combustion crater (20); (28) and a hanging central portion (3) having a pin receiving hole (36) passing through the side. 2), the central portion (32) being the second side surface (38) of the cooling gallery (30). and a side wall (22) extending between it and the cooling gallery (30). and a crown (11) having a bottom surface (40) located above the pin receiving hole (36). A method of manufacturing, a. The cylindrical outer surface (24) of the side wall (22), the ring groove (26), the top surface (18) and rough machining the combustion crater (20); b. Bottom surface (4) of crown (11) 0), and c. A certain member is inserted through the pin receiving hole (36) and the bottom surface ( 40) to stop it, and loosen one side (28, 38) of the cooling gallery (30). positioning the crown (11) by applying it to the crown; d. Combustion crater (20) and top surface (18) while positioning the crown (11) , ring groove (26), and finishing of the cylindrical outer surface (24) of the side wall (22). A method comprising: 2. The method according to claim 1, wherein the crown (1 1) is forged into the shape of an almost completed crown, and used for the rough processing stage and finishing stage. A method characterized in that it includes the step of leaving sufficient material. 3. The method according to claim 2, wherein the steel alloy contains carbon, manganese, phosphorus, and sulfur. Yellow, characterized by consisting of silicon, chromium, molybdenum, residual iron and trace elements How to do it. 4. The method of claim 1, wherein after the rough machining step about 0.030 inches. (0.75 mm) of material remains and is removed in the finishing stage. Method. 5. A method according to claim 1, in which the rough machining step includes chucking the boss (34). retaining the crown (11) by tightening with a How to do it. 6. A method according to claim 1, wherein the rough machining step comprises: a. side wall (22) gripping the cylindrical outer surface (24) near one end thereof and the other end of the side wall (22); machining a portion between the location of the two ring grooves (26) and the overlapping area; b. Grasp the rough machined portion of the cylindrical outer surface (24) and remove the cylindrical shape of the side wall (22). the remainder of the outer surface (24) between said one end and said overlapping region of one ring groove (26); a step of rough machining the c. Cutting said one ring groove (26) in the side wall (22) and rough machining of steps a and b removing any connections in the work; d. Cut the rest of the ring groove (26) A method comprising the steps of: 7. In the method according to claim 1, the boss (34) is further provided with a pin receiving hole. (36); b. finishing the pin receiving hole (36); c. Finished pin receiving hole (3 6) incorporating the bushing (37) into the d. The inner diameter of the bushing (37) installed before step c of claim 1 is and machining to its finished diameter. 8. A method of machining a crown (11) of an articulated piston (10), comprising: a circular top surface (18); a combustion crater (20) extending downward from the top surface (18); , a relatively short side wall depending from the top surface (18) and having a circumferential outer surface (24) (22) and side walls (22) and spaced below the top surface (18). A crown (11) having a plurality of ring grooves (26) arranged at positions, the crown (11) having a plurality of ring grooves (26) located at a cooling gear whose wall (22) extends adjacent the top surface (18) and the combustion crater (20); an inner surface (28) forming the first side surface of the housing (30) and a pin receiver penetrating laterally; a depending central portion (32) having a hole (36), and the side walls (22) are cylindrical. extending between the shaped side wall (22) and the cooling gallery (30) and above the pin receiving hole (36). In the method of machining a crown (11) having a bottom surface (40) located on the hand, a. Grasping the side wall (22) near one end thereof, the side wall (22) of its cylindrical outer surface (24) 22) and the area that overlaps with the position of one ring groove (26). processing; b. Grasp the rough-machined portion of the outer surface (24) and press the side wall (22) ) of the cylindrical outer surface (24) of said one end and said one ring groove (26). rough finishing another part between the areas; c. Cutting said one ring groove (26) in the side wall (22) and rough finishing of steps a and b removing any connections left by the removal operation; d. and cutting the remainder of the ring groove (26). Law. 9. A method for machining a crown of an articulated piston according to claim 8. And furthermore, a. Rough machining of the top surface (18), combustion crater (20) and bottom surface (40) and, b. finishing the bottom surface (40) of the crown (11); c. Machine a pin receiving hole (36) that extends laterally through the hanging central portion (32). processing; d. Insert a certain member into the pin receiving hole (36) and press the bottom surface (40). Place one side of the cooling gallery (30) on the locator and tighten the crown. (11) positioning the e. Burn while positioning the crown (11) Crater (20), top surface (18), cylindrical outer surface (24) and ring groove (26) and the stage of finishing the A method characterized by comprising:
JP1501366A 1988-10-21 1988-12-23 Method of manufacturing a crown for an articulated piston Expired - Lifetime JP2801049B2 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US261,457 1988-10-21
US07261457 US4847964B1 (en) 1988-10-21 1988-10-21 Method of producing a crown for an articulated piston
PCT/US1988/004605 WO1990004491A1 (en) 1988-10-21 1988-12-23 A method of producing a crown for an articulated piston

Publications (2)

Publication Number Publication Date
JPH04501087A true JPH04501087A (en) 1992-02-27
JP2801049B2 JP2801049B2 (en) 1998-09-21

Family

ID=22993392

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1501366A Expired - Lifetime JP2801049B2 (en) 1988-10-21 1988-12-23 Method of manufacturing a crown for an articulated piston

Country Status (6)

Country Link
US (1) US4847964B1 (en)
EP (1) EP0439459B1 (en)
JP (1) JP2801049B2 (en)
BR (1) BR8807924A (en)
DE (1) DE3875253T2 (en)
WO (1) WO1990004491A1 (en)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BR9001859A (en) * 1990-04-17 1991-11-12 Metal Leve Sa EMBOLO AND EMBOLO MANUFACTURING PROCESS
BR9001916A (en) * 1990-04-20 1991-11-12 Metal Leve Sa PROCESS OF OBTAINING REFRIGERATED PUMP AND REFRIGERATED PUMP
BR9004990A (en) * 1990-09-28 1992-03-31 Metal Leve Sa MANUFACTURING PROCESS OF ARTICULATED PUMP AND ARTICULATED PUMP
DE4446726A1 (en) * 1994-12-24 1996-06-27 Mahle Gmbh Process for producing a one-piece cooling channel piston
GB2297282B (en) * 1995-01-25 1997-07-23 T & N Technology Ltd Machining pistons
US5642645A (en) * 1995-09-25 1997-07-01 Teijin Seiki Boston, Inc. Hermetically sealed harmonic drive transmission manufacture
US5839352A (en) * 1996-08-07 1998-11-24 Cummins Engine Company, Inc. Articulated piston
US6155157A (en) * 1998-10-06 2000-12-05 Caterpillar Inc. Method and apparatus for making a two piece unitary piston
US6244161B1 (en) * 1999-10-07 2001-06-12 Cummins Engine Company, Inc. High temperature-resistant material for articulated pistons
DE10008559B4 (en) 2000-02-24 2007-07-26 Volkswagen Ag Method for producing pistons for a reciprocating internal combustion engine
WO2001073275A1 (en) * 2000-03-28 2001-10-04 Federal-Mogul Corporation Heavy duty piston having oil splash deflector
US6494170B2 (en) 2000-12-01 2002-12-17 Caterpillar Inc Two-piece piston assembly with skirt having pin bore oil ducts
US6487773B2 (en) * 2001-03-23 2002-12-03 Mahle Gmbh Method of making one-piece piston
US20020198075A1 (en) 2001-06-21 2002-12-26 Prucher Bryan Paul Two piece axle shaft
US6760961B2 (en) * 2002-02-12 2004-07-13 Focus: Hope Piston machining
US20080087450A1 (en) * 2006-10-11 2008-04-17 Trong-Ruey Lin Method for assembling a front cover to a bush in a pneumatic tool
DE102008018850A1 (en) * 2007-11-30 2009-06-04 Andreas Borst Piston and process for its production
US8506215B2 (en) * 2009-06-24 2013-08-13 Federal-Mogul Corporation Method of forming piston pin holes and boring system therefor
US20110030214A1 (en) * 2009-08-05 2011-02-10 Wolfgang Rein Piston assembly multiple step forming process
DE102009040120A1 (en) * 2009-09-04 2011-03-10 Mahle International Gmbh Method for producing an aluminum piston for an internal combustion engine
DE102009042655A1 (en) * 2009-09-23 2011-03-24 Bayerische Motoren Werke Aktiengesellschaft A method for producing a roof profile of an internal combustion engine piston and then produced engine piston
CN104646687A (en) * 2014-06-21 2015-05-27 柳州凯通机械有限公司 Aluminum piston machining method
CN112658596B (en) * 2020-11-16 2022-09-09 山东振挺精工活塞有限公司 Process for solving problem of unqualified parallelism of die-casting piston pin hole
US11667005B1 (en) 2022-04-27 2023-06-06 Caterpillar Inc. Method of making piston using polishing removal of thermal barrier coating (TBC) material

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE492625C (en) * 1930-02-26 Wanderer Werke Vorm Winklhofer Process for the production of pistons for internal combustion engines, especially for motor vehicles
US1475662A (en) * 1922-06-21 1923-11-27 George A Taylor Method of finishing piston-ring grooves
US2473306A (en) * 1943-01-29 1949-06-14 John H Schreiber Tandem spindle lathe
US2417132A (en) * 1943-02-01 1947-03-11 John H Schreiber Machine tool
AU503148B2 (en) * 1975-06-16 1979-08-23 Cummins Engine Company, Inc Piston with flexible heat dam
US4180027A (en) * 1977-07-20 1979-12-25 Mack Trucks, Inc. Two-piece oil-cooled piston
DE2919638A1 (en) * 1979-05-16 1980-11-20 Schmidt Gmbh Karl PISTON FOR INTERNAL COMBUSTION ENGINES
DE3222582C2 (en) * 1982-06-16 1985-10-03 Berchem & Schaberg Gmbh, 4650 Gelsenkirchen Method of manufacturing a piston crown blank by forging for an assembled piston
DE3329787A1 (en) * 1982-08-20 1984-02-23 AE PLC, Rugby, Warwickshire PISTON AND METHOD FOR THEIR PRODUCTION
GB8323843D0 (en) * 1983-09-06 1983-10-05 Ae Plc Pistons
JPS60190651A (en) * 1984-03-12 1985-09-28 Ngk Insulators Ltd Engine piston and manufacturing method thereof
DE3502248C1 (en) * 1985-01-24 1986-05-07 Berchem & Schaberg Gmbh, 4650 Gelsenkirchen Method of manufacturing a one-piece piston for an internal combustion engine by forging
EP0316330B1 (en) * 1986-08-01 1991-03-20 Ludwig Elsbett Piston upper part with incorporated support bearings for supporting the piston pin of a piston engine
US4739684A (en) * 1986-10-31 1988-04-26 The Cross Company Apparatus for finishing pistons and the like and method therefor

Also Published As

Publication number Publication date
DE3875253T2 (en) 1993-05-06
DE3875253D1 (en) 1992-11-12
US4847964B1 (en) 2000-05-09
JP2801049B2 (en) 1998-09-21
BR8807924A (en) 1991-08-13
WO1990004491A1 (en) 1990-05-03
US4847964A (en) 1989-07-18
EP0439459B1 (en) 1992-10-07
EP0439459A1 (en) 1991-08-07

Similar Documents

Publication Publication Date Title
JPH04501087A (en) How to manufacture a crown for an articulated piston
CN103619507B (en) Piston for internal combustion engine and manufacturing method thereof
EP2697016B1 (en) Method of making a piston
CN103921097B (en) Manufacturing method of hard-base soft-structure internal combustion engine connecting rod
JP5180991B2 (en) Cylinder block and method for manufacturing cylinder block
JPS5921250B2 (en) Manufacturing method for single or double flanged track tractor rollers, etc.
EP1354662A1 (en) Friction welding apparatus
EP1553313A1 (en) Connecting rod split construction
CN101501314A (en) Engine cast component having witness marks and method of machining same
JP2000061703A (en) Manufacturing method of gear with shaft
JP4550516B2 (en) Connecting rod manufacturing method and connecting rod
CN115519317A (en) Machining deformation control method for large-scale copper casting thin-wall part
JP4764666B2 (en) Tire wheel processing method and tire wheel processing gripping structure
JP2001009623A (en) Burr removing cutting tool and method for removing burr by using the cutting tool
JPH1144252A (en) Method and apparatus for manufacturing lower case of internal combustion engine
CN205437259U (en) Spline is to tooth boring grab
JPH08141849A (en) Movable sheave machining method for pulley device for continuously variable transmission
JP3805947B2 (en) Method for forming hollow forged products
JPH09206876A (en) Die for forging gear
JPH0613770Y2 (en) Machine tool rotary head
JP2004346850A (en) Cylinder block
JP3038077U (en) Combination drill
Oberg Turret Lathe Practice: A Treatise on the Application of Horizontal and Vertical Turret Lathes to Chuck and Bar Work
JP4969766B2 (en) How to remove parts
SU984771A1 (en) Tool for friction welding-on of holes

Legal Events

Date Code Title Description
R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20070710

Year of fee payment: 9

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20080710

Year of fee payment: 10

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20080710

Year of fee payment: 10

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090710

Year of fee payment: 11

EXPY Cancellation because of completion of term
FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090710

Year of fee payment: 11